Investigation of Trajectory Generation for a Mission Adaptive Planetary Entry Guidance Algorithm
Author:
Affiliation:
1. NASA Ames Research Center
2. University of California, Davis
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2012-4508
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3. Aerothermodynamic Optimization of Reentry Heat Shield Shapes for a Crew Exploration Vehicle
4. Kinney,D.,etal."ConceptualDesignofa`SHARP'-CTV,"AIAA-2001-2887,200.
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